The invention discloses a flapping-wing aircraft indoor flight path monitoring platform and an experimental method thereof, which are applied to the technical field of machinery, image acquisition anddata processing, thereby solving problems that related experimental platforms in the prior art are relatively lacked and cannot meet the requirements of researchers, so that the research of flapping-wing aircrafts is greatly hindered. The experiment platform comprises a movable flapping-wing aircraft placement platform, and can be changed at will according to the change of the experiment environment, that is, when the initial take-off position of a flight path planned by the flapping-wing aircraft according to a track changes, the flight path can be adjusted at any time to adapt to differentenvironment requirements flexibly and variably; according to the method, the performance of the ornithopter can be improved under the condition that the aerodynamics is not clear.

    本发明公开扑翼飞行器室内飞行轨迹监测平台及其实验方法,应用于机械、图像采集、数据处理技术领域,针对现有技术中相关的实验平台相对缺乏,不能够满足研究者们的需求,使得扑翼飞行器的研究也受到了极大的阻碍;本发明实验平台包含可移动的扑翼飞行器放置平台,能够根据实验环境的变化进行任意的改变,即扑翼飞行器根据轨迹规划得到的飞行路径,其初始起飞位置发生改变时,能够随时进行调整,灵活多变的适应不同的环境需求;本发明的方法可以实现在空气动力学不明确的情况下,改进扑翼飞行器的性能。


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    Title :

    Flapping-wing aircraft indoor flight path monitoring platform and experimental method thereof


    Additional title:

    扑翼飞行器室内飞行轨迹监测平台及其实验方法


    Contributors:
    WANG ZHONGLAI (author) / YU LIJUN (author) / ZHENG HAO (author) / YUE NINGYUAN (author) / ZHANG YANWEI (author)

    Publication date :

    2021-01-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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